View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58251U 26145.51847830 +.00000000 +00000-0 +84557-4 0 00001
2 58251 43.0015 211.3255 0001650 274.7278 85.3385 15.27582104 01
| Epoch (UTC): | 25 May 2026 12:26:36 |
| Eccentricity: | 0.0001650 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.3255° |
| argument of perigee: | 274.7278° |
| revolutions per day: | 15.27582104 |
| mean anomaly at epoch: | 85.3385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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